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landing)
1, 2, 3,
4, 5, 6, 7
B RSVR LO AIR PR
reservoir air pressure ≤ 22 PSI
reset if pressure ≥ 25 PSI
G (Y)(B) RSVR OVHT
fluid temperature ≥ 93 °C
(reset if temp ≤ 88 °C)
3, 4, 5, 7, 8
G (Y)(B) RSVR LO LVL
fluid quantity :
< 3.5 l (0.92 US Gal) (green-yellow)
< 2.4 l (0.63 US Gal) (blue)
FAULT lt on
associated
pump(s) pb
and on PTU
pb if Y or G
sys affected
G (Y) ENG 1(2) PUMP LO PR
pump outlet pressure ≤ 1 750 PSI
(reset if pressure ≥ 2 200 PSI)
Y ELEC PUMP LO PR
yellow system pressure ≤ 1 450 PSI
(reset if pressure ≥ 1 750 PSI) with
- Y ELEC PUMP pb at ON
- Y ENG PUMP and PTU not available
B ELEC PUMP LO PR
pump outlet pressure ≤ 1 450 PSI
(reset if pressure ≥ 1 750 PSI)
4, 5, 7, 8
B ELEC PUMP OVHT
Y ELEC PUMP OVHT 3, 4, 5, 7, 8
G (Y) SYS LO PR
system pressure ≤ 1 450 PSI
(reset if pressure ≥ 1 750 PSI)
FAULT lt
on affected
pump pb
4, 5, 7, 8 (1)
B SYS LO PR
system pressure ≤ 1 450 PSI
(reset if pressure ≥ 1 750 PSI)
SINGLE
CHIME
MASTER
CAUT
HYD
NIL 1, 4, 5,
7, 8, 10
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
HYDRAULIC
WARNINGS AND CAUTIONS
A318/A319/A320/A321 FLEET DSC-29-30 P 4/4
FCOM 19 AUG 10
Continued from previous page
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT
PHASE
INHIB
PTU FAULT
PTU not running on ground in case differential
pressure higher than 650 PSI between G and
Y system, or in flight PTU still at AUTO position
in case of G or Y reservoir low level and G or Y
system low pressure.
FAULT lt only
in case of G
or Y RSVR
LO LVL or
RSVR LO
AIR PR or
RSVR OVHT
3, 4, 5,
8, 9, 10
RAT FAULT
RAT not fully stowed or pressure present
in RAT stowing actuator or RAT pump not available
SINGLE
CHIME
MASTER
CAUT HYD
NIL 3, 4, 5,
6, 7, 8, 9
(1) Inhibited on the ground (flight phases 1, 2, 9, 10) when corresponding engine is shut down.
MEMO DISPLAY
“RAT OUT” appears green, if the ram ‐ air turbine is not fully stowed.
The color changes to amber during flight phases 1 and 2.
‐ “HYD PTU” appears green, when the power transfer unit is running.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
HYDRAULIC
ELECTRICAL SUPPLY
A318/A319/A320/A321 FLEET DSC-29-40 P 1/2
FCOM 19 AUG 10
BUS EQUIPMENT LIST
Applicable to: ALL
NORM EMER ELEC
AC DC AC
ESS
DC
ESS HOT
ENG 1 driven PUMP control DC1
ENG 2 driven PUMP control DC2
ENG 1 FIRE shut off valve X
ENG 2 FIRE shut off valve X
BLUE ELEC PUMP cpoonwtreorl AC1 X
power AC2(1) Yellow ELEC PUMP control DC2
Power Transfer Unit DC2
LEAK MEASUREMENT VALVES DC
GRND/FLT
RAT MaAnuutaol ccoonnttrrooll HHOOTT 12
(1) or from external power.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
HYDRAULIC
ELECTRICAL SUPPLY
Intentionally left blank
A318/A319/A320/A321 FLEET DSC-29-40 P 2/2
FCOM 19 AUG 10
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
Intentionally left blank
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
ICE AND RAIN PROTECTION
PRELIMINARY PAGES - TABLE OF CONTENTS
A318/A319/A320/A321 FLEET DSC-30-PLP-TOC P 1/2
FCOM 19 AUG 10
DSC-30-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
DSC-30-10 GENERAL
DSC-30-10-10 DESCRIPTION
GENERAL............................................................................................................................................................1/4
ANTI-ICING......................................................................................................................................................... 1/4
RAIN REMOVAL................................................................................................................................................. 1/4
DSC-30-20 WING ANTI-ICE
DSC-30-20-10 DESCRIPTION
DESCRIPTION.................................................................................................................................................... 1/4
　
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